| 注册
首页|期刊导航|热科学学报(英文版)|Aerodynamic Comparison between Increasing Cascade Pitch and Turning Angle in the Highly-Loaded Design

Aerodynamic Comparison between Increasing Cascade Pitch and Turning Angle in the Highly-Loaded Design

ZHOU Xun XUE Xingxu DU Xin LUO Lei WANG Songtao

热科学学报(英文版)2022,Vol.31Issue(5):1709-1722,14.
热科学学报(英文版)2022,Vol.31Issue(5):1709-1722,14.

Aerodynamic Comparison between Increasing Cascade Pitch and Turning Angle in the Highly-Loaded Design

Aerodynamic Comparison between Increasing Cascade Pitch and Turning Angle in the Highly-Loaded Design

ZHOU Xun 1XUE Xingxu 1DU Xin 2LUO Lei 1WANG Songtao1

作者信息

  • 1. School of Energy Science and Engineering,Harbin Institute of Technology,Harbin 150001,China
  • 2. Science and Technology on Diesel Engine Turbocharging Laboratory,China North Engine Research Institute,Tianjin 300270,China
  • 折叠

摘要

关键词

linear turbine cascade/highly-loaded design/secondary flow/enhancing pattern/enhancing mechanism

Key words

linear turbine cascade/highly-loaded design/secondary flow/enhancing pattern/enhancing mechanism

引用本文复制引用

ZHOU Xun,XUE Xingxu,DU Xin,LUO Lei,WANG Songtao..Aerodynamic Comparison between Increasing Cascade Pitch and Turning Angle in the Highly-Loaded Design[J].热科学学报(英文版),2022,31(5):1709-1722,14.

热科学学报(英文版)

OACSCDEISCI

1003-2169

访问量0
|
下载量0
段落导航相关论文